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You searched for: subject:"Aerodynamics--Research."
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[texts]Climb and high-speed tests of a Curtiss no. 714-1C2-12 four-blade propeller on the Republic P-47C airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807441&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 99
[texts]Maximum rates of control motion obtained from ground tests - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613620&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 48
[texts]Theories of turbulence - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807732&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence; Aerodynamics--Research
Downloads: 142
[texts]Apparatus for measurements of time and space correlation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807826&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 73
[texts]Analysis of available data on the effectiveness of ailerons without exposed overhang balance - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807486&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 122
[texts]Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003610203&ix=nu&I=0&V=D&pm=1
Keywords: Guided bombs; Aerodynamics--Research
Downloads: 110
[texts]Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614294&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 124
[texts]Review of the physical and thermodynamic properties of boric oxide - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853251&ix=nu&I=0&V=D&pm=1
Keywords: Thermodynamics--Research; Aerodynamics--Research
Downloads: 65
[texts]Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804669&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 77
[texts]Some measurements of time and space correlation in wind tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807829&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 98
[texts]On the gas dynamics of a rotating impeller - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807542&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 81
[texts]Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003600239&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 70
[texts]Kinetic treatment of the nucleation in supersaturated vapors - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807766&ix=nu&I=0&V=D&pm=1
Keywords: Atmospheric nucleation; Aerodynamics--Research
Downloads: 82
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 67
[texts]Effects of heat-capacity lag in gas dynamics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614317&ix=nu&I=0&V=D&pm=1
Keywords: Carbon dioxide; Aerodynamics--Research
Downloads: 100
[texts]Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616150&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 104
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 177
[texts]Determination of effective column length from strain measurements - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804669&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 91
[texts]Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805102&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 90
[texts]Langley full-scale-tunnel tests of the custer channel wing airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808518&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 80
[texts]Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806635&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 104
[texts]Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616345&ix=nu&I=0&V=D&pm=1
Keywords: Parachutes; Aerodynamics--Research
Downloads: 148
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 76
[texts]Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804846&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 92
[texts]Note on compressibility effects on downwash at the tail at subcritical speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003617581&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 109
[texts]Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834456&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 107
[texts]Frequency of occurrence of atmospheric gusts and of related loads on airplane structures - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808565&ix=nu&I=0&V=D&pm=1
Keywords: Airframes; Aerodynamics--Research
Downloads: 79
[texts]Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638084&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerodynamics--Research
Downloads: 146
[texts]Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003833712&ix=nu&I=0&V=D&pm=1
Keywords: Research aircraft; Aerodynamics--Research
Downloads: 107
[texts]Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616157&ix=nu&I=0&V=D&pm=1
Keywords: Wakes (Aerodynamics; Aerodynamics--Research
Downloads: 116
[texts]Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834396&ix=nu&I=0&V=D&pm=1
Keywords: Rotors (Helicopters; Aerodynamics--Research
Downloads: 102
[texts]Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 113
[texts]Effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810613&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics--Research
Downloads: 198
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 120
[texts]Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 56
[texts]Approximate determination of the power required to move control surfaces as related to control-booster design - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614183&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 93
[texts]Analysis of vertical-tail loads in rolling pull-out maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806701&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 96
[texts]Tests of a linked differential flap system designed to minimize the reduction in effective dihedral caused by power - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003631486&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Aerodynamics--Research
Downloads: 77
[texts]Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810742&ix=nu&I=0&V=D&pm=1
Keywords: Thermocouples; Aerodynamics--Research
Downloads: 90
[texts]Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804830&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 115
[texts]Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804721&ix=nu&I=0&V=D&pm=1
Keywords: Plates (Engineering; Aerodynamics--Research
Downloads: 198
[texts]Effect of initial displacement of the center support on the buckling of a column continuous over three supports - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804949&ix=nu&I=0&V=D&pm=1
Keywords: Buckling (Mechanics; Aerodynamics--Research
Downloads: 104
[texts]Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2° - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes--Hydrodynamics; Aerodynamics--Research
Downloads: 85
[texts]Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 87
[texts]Influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804754&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 175
[texts]Electromagnetic-analogy method of solving lifting-surface-theory problems - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613188&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 119
[texts]Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003612647&ix=nu&I=0&V=D&pm=1
Keywords: Projectiles, Aerial; Aerodynamics--Research
Downloads: 63
[texts]Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614166&ix=nu&I=0&V=D&pm=1
Keywords: Yawing (Aerodynamics; Aerodynamics--Research
Downloads: 179
[texts]Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806616&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 111
[texts]Simple method for estimating terminal velocity including effect of compressibility on drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638273&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 86
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